Orbital elements of FALCON HEAVY R/B
Launched | 31 October 2022 |
Flight ended | – |
Launch site | Air Force Eastern Test Range, Florida, USA |
Owner | United States |
NORAD ID | 54221 |
Date fetched |
Epoch osculation |
Inc. [°] |
Ecc. | RA asc node [hr] |
Arg Peri. [°] |
Mean anom [°] |
Mean motion [rev/day] |
Abs. mag |
Date fetched |
Epoch osculation |
Inc. [°] |
Ecc. | RA asc node [hr] |
Arg Peri. [°] |
Mean anom [°] |
Mean motion [rev/day] |
Abs. mag |
2025 Apr 05 17:56 | 2025 Mar 31 23:47:14 | 4.8895 | 0.00547 | 4.4089 | 206.5507 | 153.2899 | 0.98106 | – |
2025 Apr 04 17:56 | 2025 Mar 31 23:47:14 | 4.8895 | 0.00547 | 4.4089 | 206.5507 | 153.2899 | 0.98106 | – |
2025 Apr 03 17:56 | 2025 Mar 31 23:47:14 | 4.8895 | 0.00547 | 4.4089 | 206.5507 | 153.2899 | 0.98106 | – |
2025 Apr 02 17:57 | 2025 Mar 31 23:47:14 | 4.8895 | 0.00547 | 4.4089 | 206.5507 | 153.2899 | 0.98106 | – |
2025 Apr 01 17:56 | 2025 Mar 31 23:47:14 | 4.8895 | 0.00547 | 4.4089 | 206.5507 | 153.2899 | 0.98106 | – |
2025 Mar 31 17:56 | 2025 Mar 24 20:33:19 | 4.8718 | 0.00549 | 4.4116 | 206.3882 | 153.2899 | 0.98106 | – |
2025 Mar 30 17:57 | 2025 Mar 24 20:33:19 | 4.8718 | 0.00549 | 4.4116 | 206.3882 | 153.2899 | 0.98106 | – |
2025 Mar 29 18:56 | 2025 Mar 24 20:33:19 | 4.8718 | 0.00549 | 4.4116 | 206.3882 | 153.2899 | 0.98106 | – |
2025 Mar 28 18:57 | 2025 Mar 24 20:33:19 | 4.8718 | 0.00549 | 4.4116 | 206.3882 | 153.2899 | 0.98106 | – |
2025 Mar 27 18:56 | 2025 Mar 24 20:33:19 | 4.8718 | 0.00549 | 4.4116 | 206.3882 | 153.2899 | 0.98106 | – |
2025 Mar 26 18:57 | 2025 Mar 24 20:33:19 | 4.8718 | 0.00549 | 4.4116 | 206.3882 | 153.2899 | 0.98106 | – |
2025 Mar 25 18:57 | 2025 Mar 20 18:42:14 | 4.8614 | 0.00550 | 4.4132 | 206.2632 | 153.2899 | 0.98106 | – |
2025 Mar 24 18:57 | 2025 Mar 20 18:42:14 | 4.8614 | 0.00550 | 4.4132 | 206.2632 | 153.2899 | 0.98106 | – |
2025 Mar 23 18:58 | 2025 Mar 20 18:42:14 | 4.8614 | 0.00550 | 4.4132 | 206.2632 | 153.2899 | 0.98106 | – |
2025 Mar 22 18:58 | 2025 Mar 20 18:42:14 | 4.8614 | 0.00550 | 4.4132 | 206.2632 | 153.2899 | 0.98106 | – |
2025 Mar 21 18:57 | 2025 Mar 20 18:42:14 | 4.8614 | 0.00550 | 4.4132 | 206.2632 | 153.2899 | 0.98106 | – |
2025 Mar 20 18:57 | 2025 Mar 15 16:24:01 | 4.8483 | 0.00550 | 4.4151 | 206.1410 | 153.2899 | 0.98106 | – |
2025 Mar 19 18:57 | 2025 Mar 15 16:24:01 | 4.8483 | 0.00550 | 4.4151 | 206.1410 | 153.2899 | 0.98106 | – |
2025 Mar 18 18:56 | 2025 Mar 15 16:24:01 | 4.8483 | 0.00550 | 4.4151 | 206.1410 | 153.2899 | 0.98106 | – |
2025 Mar 17 18:56 | 2025 Mar 15 16:24:01 | 4.8483 | 0.00550 | 4.4151 | 206.1410 | 153.2899 | 0.98106 | – |
2025 Mar 16 18:56 | 2025 Mar 15 16:24:01 | 4.8483 | 0.00550 | 4.4151 | 206.1410 | 153.2899 | 0.98106 | – |
2025 Mar 15 18:56 | 2025 Mar 09 13:37:27 | 4.8327 | 0.00550 | 4.4174 | 206.0078 | 153.2899 | 0.98106 | – |
2025 Mar 14 18:56 | 2025 Mar 09 13:37:27 | 4.8327 | 0.00550 | 4.4174 | 206.0078 | 153.2899 | 0.98106 | – |
2025 Mar 13 18:57 | 2025 Mar 09 13:37:27 | 4.8327 | 0.00550 | 4.4174 | 206.0078 | 153.2899 | 0.98106 | – |
2025 Mar 11 18:56 | 2025 Mar 09 13:37:27 | 4.8327 | 0.00550 | 4.4174 | 206.0078 | 153.2899 | 0.98106 | – |
2025 Mar 10 18:56 | 2025 Mar 09 13:37:27 | 4.8327 | 0.00550 | 4.4174 | 206.0078 | 153.2899 | 0.98106 | – |
2025 Mar 09 18:57 | 2025 Mar 04 11:18:38 | 4.8202 | 0.00551 | 4.4195 | 205.9111 | 153.2899 | 0.98106 | – |